GB2577268B - Labyrinth seal for a turbine engine of an aircraft - Google Patents
Labyrinth seal for a turbine engine of an aircraft Download PDFInfo
- Publication number
- GB2577268B GB2577268B GB1815221.5A GB201815221A GB2577268B GB 2577268 B GB2577268 B GB 2577268B GB 201815221 A GB201815221 A GB 201815221A GB 2577268 B GB2577268 B GB 2577268B
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- turbine engine
- labyrinth seal
- labyrinth
- seal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/14—Two-dimensional elliptical
- F05D2250/141—Two-dimensional elliptical circular
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/293—Three-dimensional machined; miscellaneous lathed, e.g. rotation symmetrical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/447—Labyrinth packings
- F16J15/4472—Labyrinth packings with axial path
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1758917A FR3071539B1 (fr) | 2017-09-26 | 2017-09-26 | Joint d'etancheite a labyrinthe pour une turbomachine d'aeronef |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201815221D0 GB201815221D0 (en) | 2018-10-31 |
GB2577268A GB2577268A (en) | 2020-03-25 |
GB2577268B true GB2577268B (en) | 2022-11-09 |
Family
ID=60382388
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1815221.5A Active GB2577268B (en) | 2017-09-26 | 2018-09-18 | Labyrinth seal for a turbine engine of an aircraft |
Country Status (3)
Country | Link |
---|---|
US (1) | US10947857B2 (fr) |
FR (1) | FR3071539B1 (fr) |
GB (1) | GB2577268B (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3095025B1 (fr) * | 2019-04-12 | 2021-03-05 | Safran Aircraft Engines | Joint d’étanchéité à labyrinthe comportant un élément abradable à densité variable de cellules |
CN116063800B (zh) * | 2023-02-03 | 2024-05-28 | 六安江淮电机有限公司 | 一种电机用自润滑氟硅橡胶密封圈及其制备方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5429478A (en) * | 1994-03-31 | 1995-07-04 | United Technologies Corporation | Airfoil having a seal and an integral heat shield |
EP2213836A2 (fr) * | 2009-01-30 | 2010-08-04 | General Electric Company | Élément de recouvrement de chambre de rotor doté d'une ouverture pour la séparation des déchets et turbine associée |
US20120091662A1 (en) * | 2010-10-19 | 2012-04-19 | General Electric Company | Labyrinth seal system |
US8167547B2 (en) * | 2007-03-05 | 2012-05-01 | United Technologies Corporation | Gas turbine engine with canted pocket and canted knife edge seal |
US8821115B2 (en) * | 2010-08-03 | 2014-09-02 | Rolls-Royce Plc | Seal assembly |
US20160341058A1 (en) * | 2014-01-30 | 2016-11-24 | Mitsubishi Hitachi Power Systems, Ltd. | Seal structure and rotating machine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5143383A (en) * | 1984-06-04 | 1992-09-01 | General Electric Company | Stepped tooth rotating labyrinth seal |
US5639095A (en) * | 1988-01-04 | 1997-06-17 | Twentieth Technology | Low-leakage and low-instability labyrinth seal |
DE4307361A1 (de) | 1993-03-09 | 1994-09-15 | Wolfgang Mohr | Rütteltisch |
EP0777819B1 (fr) * | 1994-08-24 | 1999-10-27 | United Technologies Corporation | Joint rotatif |
US7445213B1 (en) * | 2006-06-14 | 2008-11-04 | Florida Turbine Technologies, Inc. | Stepped labyrinth seal |
US8075256B2 (en) * | 2008-09-25 | 2011-12-13 | Siemens Energy, Inc. | Ingestion resistant seal assembly |
JP5709447B2 (ja) * | 2010-09-28 | 2015-04-30 | 三菱日立パワーシステムズ株式会社 | タービン |
DE202011105609U1 (de) * | 2011-09-12 | 2011-10-13 | Alstom Technology Ltd. | Labyrinthdichtung |
JP6530918B2 (ja) * | 2015-01-22 | 2019-06-12 | 三菱日立パワーシステムズ株式会社 | タービン |
US9938840B2 (en) * | 2015-02-10 | 2018-04-10 | United Technologies Corporation | Stator vane with platform having sloped face |
GB201717015D0 (en) * | 2017-10-17 | 2017-11-29 | Rolls Royce Plc | Fluid seal |
-
2017
- 2017-09-26 FR FR1758917A patent/FR3071539B1/fr active Active
-
2018
- 2018-09-18 GB GB1815221.5A patent/GB2577268B/en active Active
- 2018-09-24 US US16/140,439 patent/US10947857B2/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5429478A (en) * | 1994-03-31 | 1995-07-04 | United Technologies Corporation | Airfoil having a seal and an integral heat shield |
US8167547B2 (en) * | 2007-03-05 | 2012-05-01 | United Technologies Corporation | Gas turbine engine with canted pocket and canted knife edge seal |
EP2213836A2 (fr) * | 2009-01-30 | 2010-08-04 | General Electric Company | Élément de recouvrement de chambre de rotor doté d'une ouverture pour la séparation des déchets et turbine associée |
US8821115B2 (en) * | 2010-08-03 | 2014-09-02 | Rolls-Royce Plc | Seal assembly |
US20120091662A1 (en) * | 2010-10-19 | 2012-04-19 | General Electric Company | Labyrinth seal system |
US20160341058A1 (en) * | 2014-01-30 | 2016-11-24 | Mitsubishi Hitachi Power Systems, Ltd. | Seal structure and rotating machine |
Also Published As
Publication number | Publication date |
---|---|
US20190093494A1 (en) | 2019-03-28 |
FR3071539A1 (fr) | 2019-03-29 |
FR3071539B1 (fr) | 2020-06-05 |
GB201815221D0 (en) | 2018-10-31 |
GB2577268A (en) | 2020-03-25 |
US10947857B2 (en) | 2021-03-16 |
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